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Section 5.— Current inspection status summary
This page should give a summary of the current inspection status of the aircraft at the time of transfer. It should list:
a)  the aircraft total time in flight hours, flight cycles, landings, calendar time, etc.;
b)  the time (in flight hours, flight cycles, landings, calendar time, etc. as appropriate) since the last major scheduled maintenance or inspection;
c)  the scheduled major inspection intervals and the time remaining to the next inspection; and
d)  the engines by position and serial number. The listing should show the time since new, cycles since new and the time and/or cycles remaining to the next life-limited part removal for each engine.
Section 6.— Summary of current status of life-limited parts
This section should contain a listing of all the airframe and powerplant life-limited components/parts installed on the aircraft at the time of transfer. The listing should contain the name of the component/part, the installed location or position of the component/part, the component/part number, the component/part serial number, the required retirement time of the component/part, the current accumulated lives (in flight hours, flight cycles, landings, calendar times, etc. as appropriate) and remaining lives before the required retirement times of the component/part is reached.
Section 7.— Current status of airworthiness directives
This section should contain a listing of each AD applicable to the aeroplane, powerplants, components and appliances. Recurring ADs should be listed separately. The listing should contain: a) the AD number and revision date of the State of the transferring operator, including a cross reference to the AD of the State of Design, if applicable; b) a concise description of the required action; c) the method of compliance; d) the time in service and the date of AD accomplishment; and e) for ADs having requirements for recurring actions the date of AD accomplishment and when the next recurring action is due (date, flight hours, flight cycles, etc.).
Section 8.— Aircraft maintenance programme integration
This section should contain the maintenance programme and a listing of each maintenance task included in this maintenance programme, the scheduled inspection interval, together with the last accomplishment applicable to the aircraft, powerplant, components and appliances. The listing should contain:
a)  the maintenance task number, including a cross reference to the TC holder’s maintenance task number in case of a different maintenance programme developed by the operator or one of its subcontracted maintenance organizations, if applicable;
b)  a cross reference to the applicable work cards;
c)  a description of the action performed; and
d)  the date of last accomplishment and the times in service if applicable.
If the maintenance/inspection programme is to be changed for the aircraft, the integration or bridging plan for the two programmes should be presented here. For an integration plan, a listing of each scheduled maintenance/inspection item under both the old and new programmes should be shown along with the method of transfer or bridging from one to the other.
Section 9.— Modifications, repairs, service bulletins
This section should contain a listing of each modification, repair or Service Bulletin embodied on the aircraft. If additional action is required, e.g. recurring inspection, this should also be indicated. The listing should contain:
a)  the modification, repair, or service bulletin number and revision date, including a cross reference to the TC holder’s modification, engineering repair approvals or service bulletin number in case of engineering orders developed by the operator or one of its subcontracted maintenance organizations, if applicable;
b)  a description of the action performed;
　
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